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公开(公告)号:US10894611B2
公开(公告)日:2021-01-19
申请号:US15911836
申请日:2018-03-05
Applicant: Airbus Operations S.A.S.
Inventor: Didier Deletoille , Frédéric Forget
Abstract: A lightning protection system of an aircraft when it is electrically powered on the ground by a generator set is described. Such an aircraft consequently includes a fuselage and a connecting connector to allow the connection to the generator set. The connecting connector includes a frame, male electrical contacts protruding on either side of said frame, and a lightning protection system inserted between the male electrical contacts and electrical elements of the aircraft. The protection system includes peak-clipping devices for clipping an electrical signal and a printed circuit having conductive tracks linking the male electrical contacts to the peak-clipping devices.
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公开(公告)号:US20180257789A1
公开(公告)日:2018-09-13
申请号:US15911836
申请日:2018-03-05
Applicant: Airbus Operations S.A.S.
Inventor: Didier Deletoille , Frédéric Forget
CPC classification number: B64D45/02 , B64F1/36 , B64F1/364 , H01R13/6666 , H02G13/20 , H02H9/042 , H02J7/0029 , H02J7/0042 , H02J7/027
Abstract: A lightning protection system of an aircraft when it is electrically powered on the ground by a generator set is described. Such an aircraft consequently includes a fuselage and a connecting connector to allow the connection to the generator set. The connecting connector includes a frame, male electrical contacts protruding on either side of said frame, and a lightning protection system inserted between the male electrical contacts and electrical elements of the aircraft. The protection system includes peak-clipping devices for clipping an electrical signal and a printed circuit having conductive tracks linking the male electrical contacts to the peak-clipping devices.
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